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一种改进的定时误差检测算法 总被引:1,自引:0,他引:1
定时恢复环路是数字接收机同步模块的一个重要组成部分,Gardner算法以实现结构简单,不敏感于载波相位,独立于调制方式等优点作为定时误差检测算法广泛应用于数字接收机的定时恢复环路中。鉴于Gardner算法在数字接收机定时同步中的广泛应用,并通过比较Gardner算法及其改进算法的定时抖动和捕获性能,研究了一种改进的Gardner定时误差检测算法。仿真结果表明,该算法对于MPSK恒包络的调制信号定时抖动性能有很明显的改善,并且在小滚降因子下改善仍然成立,但是对于16QAM非恒包络的调制信号改善不理想。 相似文献
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UUV平台自噪声会对舷侧阵产生干扰,从而影响其探测性能,本文针对平台尾部自噪声源的直达噪声和海面反射噪声,提出了基于近场聚焦逆波束形成的平台噪声自适应抵消方法。文中利用UUV平台设计参数、深度以及运动姿态信息对尾部自噪声传播到舷侧阵的路径建立几何模型,并分析了影响该路径的因素;通过该模型,平台尾部自噪声能够实时自适应地通过聚焦波束形成被估计出来,从而在舷侧阵的接收信号中实现干扰抵消。仿真结果与海试实验数据处理结果表明,该方法能够有效抑制尾部自噪声干扰,显著提高UUV探测弱目标的能力。 相似文献
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Airfoil self-noise is a common phenomenon for many engineering applications. Aiming to study the underlying mechanism of airfoil self-noise at low Mach number and moderate Reynolds number flow, a numerical investigation is presented on noise generation by flow past NACA0018 airfoil. Based on a high-order accurate numerical method, both the near-field hydrodynamics and the far-field acoustics are computed simultaneously by performing direct numerical simulation. The mean flow properties agree well with the experimental measurements. The characteristics of aerodynamic noise are investigated at various angles of attack. The obtained results show that inclining the airfoil could enlarge turbulent intensity and produce larger scale of vortices. The sound radiation is mainly towards the upper and lower directions of the airfoil surface. At higher angle of attack, the tonal noise tends to disappear and the noise spectrum displays broad-band features. 相似文献
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